A Blended Sliding Mode Control with Linear Quadratic Integral Control based on Reduced Order Model for a VTOL System.

 

Authors
Camacho Quintero, Oscar Eduardo
Format
Article
Status
publishedVersion
Description

In this paper, a Sliding Mode Control with chattering reduction based on reduced order model using Linear Quadratic Integral Control as sliding surface, is implemented to One Degree of Freedom Vertical Take-Off Landing System (VTOL). The controller performance is measured using Integral of the Square Error index by simulation and real tests. Finally, the Sliding Mode Control with a Linear Quadratic Integral Control as sliding surface performance for reference tracking and, robustness against VTOL system physical parameter uncertainties and external disturbances are verified by experimental results.
https://www.researchgate.net/publication/318310662_A_Blended_Sliding_Mode_Control_with_Linear_Quadratic_Integral_Control_based_on_Reduced_Order_Model_for_a_VTOL_System

Publication Year
2017
Language
eng
Topic
SLIDING MODE CONTROL
LQI
REDUCED ORDER MODEL
ISE INDEX
Repository
Repositorio SENESCYT
Get full text
http://repositorio.educacionsuperior.gob.ec/handle/28000/4641
Rights
openAccess
License
closedAccess